Design and Evaluation of a High-Lift, Thick Airfoil for UAV Applications.
Author:
Affiliation:
1. Dept. of Aerospace Engineering and Engineering Mechanics, San Diego State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-292
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4. McGheeR.J.andBeasleyW.D."Wind-TunnelResultsforaModified17-Percent-ThickLow-SpeedAirfoil Section",NACATechnicalPaper 1919,1981.
5. Development of two-element NLF airfoils for long endurance flight
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